Boundary-Layer Transition on the N.A.C.A. 0012 and 23012 Airfoils in the 8-Foot High-Speed Wind Tunnel
1940-01-01
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Englisch
Engineering Index Backfile | 1936
|High-speed wind-tunnel tests of NACA 23012 and 23012-64 airfoils
Engineering Index Backfile | 1941
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